KUIPER-00111, 65149
Orbit data source: Space-Track
KUIPER-00111, 65149 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Mon, 11 Aug 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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65149 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational Commercial Communications
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.4 m
Radar Cross Section
2.326 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00111
1 65149U 25171T 26171.44161293 .00003141 00000-0 44097-3 0 9994
2 65149 51.8975 78.6495 0000846 105.6398 254.4658 14.79920704 47896Epoch: 2026-06-20T10:35Z
TLE epoch observation values (Epoch: 2026-06-20T10:35:55.357Z)
Latitude
0.00002°
Longitude
11.01267°
Altitude
630.48 km
Speed
7.544 km/s
True Right ascension
05h 14m 35s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
08:32:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.619 km
Perigee altitude
629.433 km
Semi-major axis
7,008.163 km
Eccentricity
0.00008
Inclination
51.8975°
RAAN
78.6495°
Arg. of periapsis
105.6398°
True anomaly
254.45646°
Mean anomaly
254.4658°
Eccentric anomaly
254.46113°
Mean motion
3.69945 °/min
Orbital period
97.31 mins
BSTAR
0.00044097
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Other satellites on launch #171 in the year 2025 (2025-08-11 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.KUIPER-00111 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-20 22:10:59.449Z | 273.898° WNW | 2026-06-20 22:14:59.449Z | 337.033° NNW | 27.244° | 2026-06-20 22:18:59.449Z | 39.152° NE |
| 4 mins | 2026-06-20 23:55:59.449Z | 332.341° NNW | 2026-06-20 23:57:59.449Z | 4.8° NNE | 17.059° | 2026-06-20 23:59:59.449Z | 33.832° NE |
| 6 mins | 2026-06-21 01:37:59.449Z | 337.299° NNW | 2026-06-21 01:39:59.449Z | 12.931° NNE | 23.379° | 2026-06-21 01:43:59.449Z | 75.652° E |
| 7 mins | 2026-06-21 03:18:59.449Z | 307.644° NW | 2026-06-21 03:21:59.449Z | 305.114° NW | 44.616° | 2026-06-21 03:25:59.449Z | 129.224° SE |
| 4 mins | 2026-06-21 19:10:59.449Z | 155.533° SSE | 2026-06-21 19:11:59.449Z | 138.33° SSE | 19.676° | 2026-06-21 19:14:59.449Z | 88.903° E |
| 7 mins | 2026-06-21 20:50:59.449Z | 248.302° W | 2026-06-21 20:53:59.449Z | 357.098° N | 41.553° | 2026-06-21 20:57:59.449Z | 47.901° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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